View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48137U 26145.43380477 +.00000000 +00000-0 +60348-4 0 00005
2 48137 53.1609 158.4005 0001276 91.4896 268.6251 15.31704323 04
| Epoch (UTC): | 25 May 2026 10:24:40 |
| Eccentricity: | 0.0001276 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 158.4005° |
| argument of perigee: | 91.4896° |
| revolutions per day: | 15.31704323 |
| mean anomaly at epoch: | 268.6251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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